Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10782
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-16 DEB.
Object identification
Identified? True
Debris? True
Object name: SL-16 DEB
International designator: 1995-058D
Object number (NORAD): 23707
Object ID (CCSDS): 23707
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.924 minutes
Inclination: 70.995 deg
SMA: 7369.041 km
Apoapsis: 1142.789 km
Periapsis: 839.024 km
RAAN: 207.5714 deg
Eccentricy: 0.0206109
Argument of periapsis: 333.0537 deg
Mean anomaly: 136.2888 deg
Mean motion: 13.72417641 rev/day
Mean motion (dot): 0.00000047 rev/day2
B* drag term: 0.000084786 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 1:50 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23707U 95058D 25127.57666769 .00000047 00000-0 84786-4 0 9993
TLE line 2: 2 23707 70.9950 207.5714 0206109 333.0537 136.2888 13.72417641477717
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
Associated space launch
Second generation ELING satellite
SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 17’, on board a Zenit-2 space rocket.
The launch took place on Oct. 31, 1995, 8:19 p.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 17
Agency: N/A
Status: Launch Successful
Launch date: Oct. 31, 1995, 8:19 p.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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